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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The degree of reaction is usually kept ________ for all types of axial flow compressors.

0.5
0.3
0.2
0.4

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Compressors, Gas Turbines and Jet Engines
The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called

Slip factor
None of these
Velocity coefficient
Velocity factor

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor resembles

Centrifugal pump
Turbine
Reciprocating pump
Sliding vane compressor

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Compressors, Gas Turbines and Jet Engines
The following property is most important for material used for gas turbine blade

Creep
Fatigue
Corrosion resistance
Toughness

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Compressors, Gas Turbines and Jet Engines
Gas turbine blades are given a rake

In the direction of motion of blades
Opposite to the direction of motion of blades
Equal to zero
Depending on the velocity

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Compressors, Gas Turbines and Jet Engines
The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio

Decreases
First decreases and then increases
Increases
First increases and then decreases

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